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Innovative Cooling for Rocket Combustion Chambers

Peichl, Jonas Stefan and Schwab, Andreas and Selzer, Markus and Böhrk, Hannah and von Wolfersdorf, Jens (2021) Innovative Cooling for Rocket Combustion Chambers. In: Future Space-Transport-System Components under High Thermal and Mechanical Loads Notes on Numerical Fluid Mechanics and Multidisciplinary Design (146). Springer Nature. pp. 51-64. doi: 10.1007/978-3-030-53847-7_3. ISBN 978-3-030-53846-0. ISSN 1612-2909.

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Official URL: https://link.springer.com/chapter/10.1007/978-3-030-53847-7_3

Abstract

Transpiration cooling in combination with permeable ceramic-matrix composite materials is an innovative cooling method for rocket engine combustion chambers, while providing high cooling efficiency as well as enhancing engine life time as demanded for future space transportation systems. In order to develop methods and tools for designing transpiration cooled systems, fundamental experimental investigations were performed. An experimental setup consisting of a serial arrangement of four porous carbon fiber reinforced carbon (C/C) samples is exposed to a hot gas flow. Perfused with cold air, the third sample is unperfused in order to assess the wake flow development over the uncooled sample as well as the rebuilding of the coolant layer. Hereby, the focus is on the temperature boundary layer, using a combined temperature/pitot probe. Additionally, the sample surface temperature distribution was measured using IR imaging. The experiments are supported by numerical simulations which are showing a good agreement with measurement data for low blowing ratios.

Item URL in elib:https://elib.dlr.de/137368/
Document Type:Contribution to a Collection
Title:Innovative Cooling for Rocket Combustion Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Peichl, Jonas StefanJonas.Peichl (at) dlr.deUNSPECIFIED
Schwab, AndreasUniversität Stuttgart, Institut für Thermodynamik der Luft- und RaumfahrtUNSPECIFIED
Selzer, MarkusMarkus.Selzer (at) dlr.dehttps://orcid.org/0000-0003-1081-5281
Böhrk, HannahHannah.Boehrk (at) dlr.deUNSPECIFIED
von Wolfersdorf, JensUniversität Stuttgart, Institut für Thermodynamik der Luft- und RaumfahrtUNSPECIFIED
Date:2021
Journal or Publication Title:Future Space-Transport-System Components under High Thermal and Mechanical Loads
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.1007/978-3-030-53847-7_3
Page Range:pp. 51-64
Editors:
EditorsEmailEditor's ORCID iD
Adams, Nikolaus A.TU MünchenUNSPECIFIED
Schröder, WolfgangRWTH AachenUNSPECIFIED
Radespiel, RolfTU BraunschweigUNSPECIFIED
Haidn, OskarTU MünchenUNSPECIFIED
Sattelmayer, ThomasTU MünchenUNSPECIFIED
Stemmer, ChristianTU MünchenUNSPECIFIED
Weigand, BernhardUniversität StuttgartUNSPECIFIED
Publisher:Springer Nature
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-030-53846-0
Status:Published
Keywords:Transpiration cooling, Thermodynamics, Computional Fluid Dynamics, Rocket Combustion Chambers
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Space System Integration
Deposited By: Peichl, Jonas Stefan
Deposited On:08 Dec 2020 14:49
Last Modified:14 Dec 2020 09:59

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